EP4389595A3 - Flugzeugflügelanordnung - Google Patents

Flugzeugflügelanordnung Download PDF

Info

Publication number
EP4389595A3
EP4389595A3 EP23212980.9A EP23212980A EP4389595A3 EP 4389595 A3 EP4389595 A3 EP 4389595A3 EP 23212980 A EP23212980 A EP 23212980A EP 4389595 A3 EP4389595 A3 EP 4389595A3
Authority
EP
European Patent Office
Prior art keywords
aircraft wing
wing assembly
drive mechanism
lift device
high lift
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP23212980.9A
Other languages
English (en)
French (fr)
Other versions
EP4389595B1 (de
EP4389595A2 (de
Inventor
Peter Kelly
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations Ltd
Original Assignee
Airbus Operations Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations Ltd filed Critical Airbus Operations Ltd
Publication of EP4389595A2 publication Critical patent/EP4389595A2/de
Publication of EP4389595A3 publication Critical patent/EP4389595A3/de
Application granted granted Critical
Publication of EP4389595B1 publication Critical patent/EP4389595B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Connection Of Plates (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
EP23212980.9A 2022-11-29 2023-11-29 Flugzeugflügelanordnung Active EP4389595B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2217919.6A GB2624887A (en) 2022-11-29 2022-11-29 Aircraft wing assembly

Publications (3)

Publication Number Publication Date
EP4389595A2 EP4389595A2 (de) 2024-06-26
EP4389595A3 true EP4389595A3 (de) 2024-08-14
EP4389595B1 EP4389595B1 (de) 2026-07-22

Family

ID=84889514

Family Applications (1)

Application Number Title Priority Date Filing Date
EP23212980.9A Active EP4389595B1 (de) 2022-11-29 2023-11-29 Flugzeugflügelanordnung

Country Status (4)

Country Link
US (1) US12479569B2 (de)
EP (1) EP4389595B1 (de)
CN (1) CN118107777A (de)
GB (1) GB2624887A (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4385887B1 (de) * 2022-12-14 2026-02-18 Airbus Operations GmbH Lasteinführungssystem und verfahren zur herstellung eines lasteinführungssystems
GB2703006A (en) * 2024-11-29 2026-07-08 Airbus Operations Ltd Split riblet
DE102024137083A1 (de) * 2024-12-11 2026-06-11 Airbus Operations Gmbh Vorflügel-hohlkehlen-fülleinrichtung für einen vorflügel eines luftfahrzeugs, zugehöriger vorflügel, tragfläche, luftfahrzeug und verfahren zum rekonfigurieren einer tragfläche
GB2703021A (en) * 2024-12-16 2026-07-08 Airbus Operations Ltd Enclosure device
US20260175963A1 (en) * 2024-12-20 2026-06-25 The Boeing Company System and method for supporting a leading edge of a wing of an aircraft

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070102587A1 (en) * 2005-11-07 2007-05-10 The Boeing Company Wing leading edge slat system
US20100065687A1 (en) * 2008-04-02 2010-03-18 Airbus Uk Limited Aircraft structure
US11427302B2 (en) * 2019-04-01 2022-08-30 Yaborã Indústria Aeronáutica S.A. Closure fairings for wing leading edge slat track openings

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4285482A (en) * 1979-08-10 1981-08-25 The Boeing Company Wing leading edge high lift device
US4469297A (en) * 1980-08-13 1984-09-04 The Boeing Company Extendible airfoil cable drum track assembly
EP0045988B2 (de) 1980-08-13 1993-10-06 The Boeing Company Führungsschienenanordnung für ausfahrbare Flügelklappen
US4471928A (en) * 1980-08-13 1984-09-18 The Boeing Company Extendible airfoil track assembly
US4687162A (en) 1985-06-25 1987-08-18 The Boeing Company Apparatus for supporting an aircraft guide track for a movable airfoil
US5927656A (en) 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
US9522512B2 (en) * 2010-08-17 2016-12-20 The Boeing Company Methods for making composite structures having composite-to-metal joints
ES2426111B1 (es) * 2012-04-17 2015-03-24 Airbus Operations S.L. Interfaz para superficie de sustentación de aeronave
GB2557274A (en) * 2016-12-02 2018-06-20 Airbus Operations Ltd Aerofoil structure components
WO2018197265A1 (en) 2017-04-28 2018-11-01 Airbus Operations Gmbh Wing for an aircraft
EP3395679B1 (de) 2017-04-28 2021-09-01 Airbus Operations GmbH Flügel für ein flugzeug
US10974816B2 (en) * 2017-09-28 2021-04-13 The Boeing Company High-fowler flap actuation apparatus and related methods
GB2571508A (en) * 2017-12-13 2019-09-04 Airbus Operations Ltd Aerofoil structures
WO2021037981A1 (en) 2019-08-30 2021-03-04 Airbus Operations Gmbh Leading edge assembly, wing, and aircraft
FR3103175A1 (fr) * 2019-11-18 2021-05-21 Airbus Élément aérodynamique, en particulier pour aéronef, comportant deux pièces aérodynamiques formant une jonction de profil ascendant.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070102587A1 (en) * 2005-11-07 2007-05-10 The Boeing Company Wing leading edge slat system
US20100065687A1 (en) * 2008-04-02 2010-03-18 Airbus Uk Limited Aircraft structure
US11427302B2 (en) * 2019-04-01 2022-08-30 Yaborã Indústria Aeronáutica S.A. Closure fairings for wing leading edge slat track openings

Also Published As

Publication number Publication date
EP4389595B1 (de) 2026-07-22
US12479569B2 (en) 2025-11-25
EP4389595A2 (de) 2024-06-26
GB2624887A (en) 2024-06-05
GB202217919D0 (en) 2023-01-11
CN118107777A (zh) 2024-05-31
US20240174351A1 (en) 2024-05-30

Similar Documents

Publication Publication Date Title
ES2646445T3 (es) Generador de vórtice retráctil
EP1607324B8 (de) Vorflügel für ein Flugzeug und entsprechende Verfahren
US20110127386A1 (en) Trailing edge flap
CN211592909U (zh) 一种可收放式襟翼辅助增升装置
DE602005015123D1 (de) Flügelspitzenvorrichtungen
ATE513735T1 (de) Flügel
EP4484282A3 (de) Flügel für ein flugzeug
CN101765539A (zh) 变换襟翼驱动门
WO2005049424A3 (en) Aircraft lift device for low sonic boom
RU2008138594A (ru) Крыло летательного аппарата (варианты), отклоняемый предкрылок и летательный аппарат
CN104692283A (zh) 一种升降机构
CN102285601A (zh) 一种平台吊机用旋转式带限位开关缓冲器
EP4282752A3 (de) Flugzeugfahrwerksanordnung
CN208081862U (zh) 一种可收放的航模起落架
CN106335678B (zh) 一种铝材贴膜机的保护膜分断机构
CN207683769U (zh) 一种翼展方向长度可变机翼及具有其的飞机
CN104477375A (zh) 一种可调平尾
CN108710014B (zh) 电表开盖机构及其开盖方法、表计加工物流系统
CN207234725U (zh) 一种移动式光伏发电装置
CN216233072U (zh) 一种飞机后襟翼滑轨的定位装置
CN209036609U (zh) 一种具有预压功能的裁切装置
EP2604511A3 (de) Flugzeugflügelanordnung
CN103640695A (zh) 新型垂直升降固定翼飞机
CN203430340U (zh) 用于双层玻璃窗户的平推式遮阳装置
CN106863992B (zh) 一种液晶面板防止裂屏的吸附机构

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC ME MK MT NL NO PL PT RO RS SE SI SK SM TR

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC ME MK MT NL NO PL PT RO RS SE SI SK SM TR

RIC1 Information provided on ipc code assigned before grant

Ipc: B64C 3/28 20060101ALI20240711BHEP

Ipc: B64C 3/18 20060101ALI20240711BHEP

Ipc: B64C 9/22 20060101AFI20240711BHEP

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20250214

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20260212

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC ME MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: F10

Free format text: ST27 STATUS EVENT CODE: U-0-0-F10-F00 (AS PROVIDED BY THE NATIONAL OFFICE)

Effective date: 20260722

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602023020169

Country of ref document: DE